• 전기학회논문지
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• 제64권2호
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• pp.289-296
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• 2015

In this paper, we propose the nonlinear control based on singular perturbation theory for position tracking and yaw regulation of planar motor. Singular perturbation theory is characterized by the existence of slow and fast transients in the system dynamics. The proposed method consists of auxiliary control to decouple error dynamics. We develop model reduction with control input. Also, we derIve decoupled error dynamics with auxiliary input. The controller is designed in order to guarantee the desired position and yaw regulation without current feedback or estimation. Simulation results validate the effect of proposed method.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집A
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• pp.252-257
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• 2001

With the help of newly arrived technology such as PC clustering, molecular dynamics (MD) seems to be promising for large-scale materials simulations. A cost-effective cluster is set up using commodity PCs connected over Ethernet with fast switching devices and free software Linux. Executing MD simulations in the parallel sessions makes it possible to carry out large-scale materials simulations at acceptable computation time and costs. In this study, the MD computer code for fracture simulation is modified to comply with MPI (Message Passing Interface) specification, and runs on the PC cluster in parallel mode flawlessly. It is noted that PC clusters can provide a rather inexpensive high-performance computing environment comparing to supercomputers, if properly arranged.

• 한국광학회지
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• 제8권6호
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• pp.471-475
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• 1997

본 논문에서는 에르븀 첨가 광섬유 증폭기를 이용하여 단일 채널을 증폭할 때의 이득 동특성(gain dynamics)과 다채널을 증폭할 때의 이득 동특성에 대해 논의하였다. 여러 개의 에르븀 첨가 광섬유 증폭기가 연결된 증폭기 체인에서 채널 수의 변화에 의해 입력 광파워가 변할 때의 출력 광파워의 과도 현상(power transients)을 측정하고, 이를 $\mu\textrm{s}$ 이하의 응답 시간을 갖는 펌프 광파워 조절 회로를 이용하여 억제하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.257-261
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• 2004

Computational fluid dynamics analysis was carried out for thermo-chemical flow field in Arcjet thruster with mono-propellant Hydrazine ($N_2$H$_4$) as a working fluid. The theoretical formulation is based on the Reynolds Averaged Navier-Stokes equations for compressible flows with thermal radiation. The electric potential field governed by Maxwell equation is loosely coupled with the fluid dynamics equations through the Ohm heating and Lorentz force. Chemical reactions were assumed being infinitely fast due to the high temperature field inside the arcjet thruster. An equilibrium chemistry module for nitrogen-hydrogen mixture and a thermal radiation module for optically thin media were incorporated with the fluid dynamics code. Thermo-physical process inside the arcjet thruster was understood from the flow field results and the performance prediction shows that the thrust force is increased by amount of 3 times with 0.6KW arc heating.

• 한국안전학회지
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• 제28권1호
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• pp.57-62
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• 2013

Aerodynamic characteristics of cross section shape is an important parameter for the wind response and structural stability of long span bridges. Numerical simulation methods have been introduced to estimate the aerodynamic characteristics for more detailed flow analysis and cost saving in place of existing wind tunnel experiment. In this study, the computational fluid dynamics(CFD) simulation and large eddy simulation( LES) technique were used to estimate lift, drag and moment coefficients of four cross sections. The Strouhal numbers were also determined by the fast Fourier transform of time series of the lift coefficient. The values from simulations and references were in a good agreement with average difference of 16.7% in coefficients and 8.5% in the Strouhal numbers. The success of the simulations is expected to attribute to the practical use of numerical estimation in construction engineering and wind load analysis.

• Journal of Astronomy and Space Sciences
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• 제32권1호
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• pp.1-11
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• 2015

Earth's magnetopause separating the fast and often turbulent magnetosheath and the relatively stagnant magnetosphere provides various forms of free energy that generate low-frequency surface waves. The source mechanism of this energy includes current-driven kinetic physical processes such as magnetic reconnection on the dayside magnetopause and flux transfer events drifting along the magnetopause, and velocity shear-driven (Kelvin-Helmholtz instability) or density/pressure gradient-driven (Rayleigh-Taylor instability) magnetohydro-dynamics (MHD) instabilities. The solar wind external perturbations (impulsive transient pressure pulses or quasi-periodic dynamic pressure variations) act as seed fluctuations for the magnetopause waves and trigger ULF pulsations inside the magnetosphere via global modes or mode conversion at the magnetopause. The magnetopause waves thus play an important role in the solar wind-magnetosphere coupling, which is the key to space weather. This paper presents recent findings regarding the generation of surface waves (e.g., Kelvin-Helmholtz waves) at the Earth's magnetopause and analytic and observational studies accountable for the linking of the magnetopause waves and inner magnetospheric ULF pulsations, and the impacts of magnetopause waves on the dynamics of the magnetopause and on the inner magnetosphere.

• 반도체디스플레이기술학회지
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• 제18권4호
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• pp.25-29
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• 2019

Microstructure pattern generation on light guides in backlight unit (BLU) is an essential process for designing flat panel display, but efficient designing algorithm is still limited to achieve uniform luminescence while maintaining fully random distribution to avoid interference effects. In this study, a molecular dynamics model based pattern generation algorithm has been developed. The proposed algorithm allows a fast and efficient distribution of patterns at specified density within the user-defined computational cells, and its efficiency and performance has been demonstrated with sample cases.

• 대한환경공학회지
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• 제35권10호
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• pp.710-716
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• 2013

대기 오염, 기후 변화 등 환경 문제와 자원 고갈로 인해 화석 연료를 대체할 에너지에 많은 관심이 집중되고 있다. 폐바이오매스의 에너지화 분야에서도 다양한 연구가 이루어지고 있다. 폐목질계 바이오매스의 급속열분해는 바이오매스 에너지화 기술 중 하나로 액상 연료를 생산할 수 있다. 바이오매스의 급속열분해에는 주로 기포유동층 반응기가 쓰이고 있으며, 기포유동층 급속열분해 반응기에서는 반응물에 열을 효과적으로 전달하기 위하여 고체입자의 유동매체를 이용한다. 이러한 기포유동층 반응기에서 유동층 내 고체 입자의 움직임과 혼합은 기포의 거동에 영향을 받는다. 이로 인해 열전달 현상이 달라지고 결과적으로는 폐목질계 바이오매스의 급속열분해 반응 속도가 변한다. 따라서 본 연구에서는 기포유동층 반응기 내부의 수력학적 특성과 폐목질계 바이오매스 급속열분해 반응에 관한 연구를 수행하였다. 반응기내의 기체-고체 유동에 대해 Eulerian-Granular 방법을 사용하여 반응기를 시뮬레이션 하였으며, two-stage semi-global reaction model로 폐바이오매스의 급속 열분해반응을 모사하였다. 결과를 살펴보면, 유동층 내에서 기포들이 생성되고 상승하면서 크기가 증가한다. 이러한 기포의 거동에 의해 기포 주위의 고체 입자는 여러 방향으로 움직이게 된다. 고체 입자상의 활발한 움직임으로 바이오매스 입자가 유동층에 골고루 퍼져 일차 반응이 유동층 전반에서 일어난다. 그리고 일차 반응 중 타르가 생성되는 반응 속도가 가장 높게 나타난다. 그 결과 기체상 생성물 중 타르가 약 66 wt.%로 가장 많이 발생한다. 반면 이차 반응은 유동층에서보다 freeboard에서 더 많이 일어난다. 따라서 기포의 거동이나 입자의 움직임에 의한 영향은 일차 반응보다 상대적으로 적을 것으로 판단된다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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• pp.482-485
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• 1996

We design a homing guidance law based on the proportional navigation for the fast-rolling, single-axis control missiles and analyse the misdistance of the designed guidance system. The guidance law includes a compensation scheme which compensates for the phase-shift between the commanded and achieved acceleration which is peculiar to the fast rolling airframe with single-axis control. In the error analysis of the guidance system, we calculate the misdistance with respect to the target maneuver on the 3-dimensional space via direct simulations. Also, we conduct adjoint simulation on the 2-dimensional plane in case that phase-shift is perfectly compensated. Finally we approximate the linear time-varying dynamics of the missile with autopilot to a linear time-invarient system, and as a result we can find the misdistance as a closed-form.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2011년도 추계학술대회 초록집
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• pp.42.1-42.1
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• 2011

NREL NWTC Deside codes are analyzed and introduced to develop the system performance simulation program for wind turbine generator systems. In this paper, The FAST performing multi-body and flexible body dynamics, control and the AeroDyn calculating aerodynamic forces with airfoil data and wind data are explained. Furthermore, initialization and process for transfer of aerodynamic force between AeroDyn and FAST at each time step are also introduced.